Flying-machine.



R. B. SWANK.

FLYING MACHINE.

'APPLIGATION FILED JUNE 1, 1911.

1,020,628. l Patented Mar.19,19 12.

6 SHEETS-SHEET 1.

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V v um arianna R. B. SWANK.'

FLYING MACHINE.

APPLICATION FILED JUNE l, 1911.

Patented Marl. 19, 1912.

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R. B. SWANK..

FLYING MACHINE.

ABPLIOATION. FILED JUNE 1,1911.

Patented Mar. 19, 1912.

6 SHEETS-SHEEP 3.

ghwcnroz 136,@ 5022 yczzz-/a' R. B. SWANK. FLYING MACHINE.

APPLICATION FILED JUNE 1,1911,

Patented Mar. 19,1912.

6 SHEETS-SHEET 4.

Stroznega R. vB. SWANK.

FLYING MACHINE.

APPLICATION FILED JUNE 1, 1911. Patented Mar. 19, 1912.

atromwao R. B. SW ANK. FLYING MACHINE. APPLICATION FILED JUNE 1, 1911.

1,020,628, Patnted Ia 1-.n19,1912- swims-Sunnis.

Hozump UNTTED sTATEs PATENT' oEEIcE.

EEUBENl B. swANx, .or DArToN, oHIo.

FLYING-MACHINE.

To all whom t may concern:

Be it known that I,- REUBE'N B. SWANK, a citizen of the 'United States, residing at Dayton,.in the county of Montgomery and State of Ohio, have invented certain new.

and vuseful, Improvements vin Flying-Machines; and I do declare the following to be a full, clea, vand exact description of the invent-ion, such as will enable others skilled in the art to which it appe'rtains. to make and use the same.

4This invention relates to improvements in' flying machines.

Une object ofthe invention )is to provide a fiying machine having an improved c onstruction and Aarrangement of supporting' planes whereby the machine may be mamtained in a horizontal position during iiight, means being .provided whereby said planes may be independently adjusted to direct the machine upwardly or downwardly lor adjusted in 'unison to form a parachute whereby the m'achine may be lowered without danger should the working parts of the same becomedisabled.

Another object is to provide a flying machine having an improved construction and .arrangement of rotary liftingv planes by means of which the machine may be quickly elevated straight up, said planes having means whereby the same may be tilted for- -wardly to assist in propelling the machine in a forward direction.

A further" object is to provide animproved construction 'and arrangement of' steering mechanism whereby the machine may be perfectly controlled by the aviator. vWith these and other objects in view, the invention consists of certain novel features of construction, combination and arrange.

. ment of arts as will be more fully described and partlcula'rly pointed out inthe appended l claims;

In the accompanying dllawingsrFi'gure 1 is a rear end/view of my lmproved airship;

.. Fig. 2 is a top plan view thereof; Fig. 3 is f a side elevation with parts brokenl away and in section ,"Fig. 4 is a vertical cross sectional View on an enlarged scale through the center ofthe machine: Fig. 5 is a' horizontal seetional view on the line 5.-'-5 of Fig. 4 5-Fig. 6 is ahorizontal sectional View taken immediatelyzabovethe driving shafts of the ro- 'tary lifting planes; Fig. 7 is adetail .side View `Aof the. innerportion of the steering i `1 rlieehauism; Fig. 8 is av detail. fragmentary Specication of Iietters Patent. I

sectional View -of the rear portion'iof the steering mechanism on the line' 8-8 of Fig. 6; Fig. 9 is a similar view on the line 9 9- of Fig. 6; Fig. 10 is a detail vertical sectional lView of the clutch mechanism for throwing the connecting gears ofthe horizontal plane operating shafts into and out of operation whereby said planes may be operated independently or in unison; Fig. 11 is an enlarged detail side view ofone of the rotary liftingplanes; Fig. 12 ,isa detail sectional view of the upper end of the supporti-ng andv operating shaft of one of the rotary lifting planes; Fig.- 13` is a detail y y Patented Mar. 19, 1912. .Applicationled June -1, 1911. Serial No. 630,671. y A

fragmentary side viewof the outer end of I one of the lower supporting members of the rotary lifting planes and the supporting and operating shafts of said planes; Fig. 14 is a sectional view'ofone of the locking devices for holding. the horizontal sustaining planes in theirV adjustedv position; Fig. 15 is an enlarged detail cross sectional .view

through the adjusting mechanism for the.

upper ends of the rotary plane .supporting shafts taken on the line 15`-15 of Fig. 11.

Referring more particularly to the draw ings, 1 `denotes the main supporting frame of the machine, said frame comprismg longltudmally disposed side bars 2 which are curved upwardly at their forward ends and are connected together-at said ends by the shaft 3 of a steering mechanism hereinafter described. The bars 2 are connected together f at their rear ends by a cross bar 4 and have arranged between their rear endsa platform 5.- The rear portionf of the frame 1 is preferably provided with pairs ofl supporting wheels 6 whereby the machine is adapted to travel on the ground.

Secured to the side bars ofthe frame are upwardly projecting planesupporting bars 7 which are connected Vtogether at their :upper ends by crossedV braces -8 and are -braced by suitable inclined trussed brace 'bars 9.v To the upper ends of the bars ,7

are hingedly connectedthe inner ends of front and rear sustaining planes 10 and 11 which may -be Yof any suitable construction, .but which are preferably in 'the form of fabric covered frames. The planes 10`and 11 are adjustably supported at their outer ends by pairs of inclinedsupporting bars 12 and ,13 Fig. 3 having on: theouter edges -of their` lower ends rack teeth 14. The @toothed 'lower ends of the bars 12 are en-v with spur'gears 15 on the opposite ends of a plane operating sha'ft 16 whereby the plane 10 may be raised or lowered. The lower ends of the bars 13 are engaged with gears 1T fixed on the outer end of a plane operating shaft 18 by means of which the plane 1 1 is raised and lowered. `The lower ends of the bars 12 and 13 are held in operative engagement with the gears 15 and 17 by suitable guide casings 19 pivotally mounted on the. ends of the shafts 16 and 18 as shown.

The shafts 16 and 18 are each provided with means forV turning the same in the desired direction for adjusting the planes operated thereby and for locking the same against movement whereby said planes are secured in `their adjusted position. The operating and locking means for said shafts comprise stationaryl disks or plates 2O which are preferably formed integral with the bearings 21 of the shaft and are rigidly secured to "the supporting bars 7 of the planes. In the the inner sides of the disksl 20 are annular series of locking Keyed or otherorplates notches or recesses 22.

lwise fixedly secured to the shafts 16 and l18 adjacent to and adapted to coact with the disks 20 are crank disks or plates 23 to which are secured laterally extending crank handles 24 whereby said disks and the shaft to which they are secured may be turned in the desired direction. Also arranged on the disks 23 are locking pins 240, Fig. 14, the in-Y` ner ends of which are loosely engaged with transverse passages 25 formed in the disks 23. The outer portions of the pins 240 are slidably engaged with casings 26 and have arranged thereon in said casings, pin projecting springs 27 the outer end of which, engage the outer ends of the casing andthe opposite ends engage stop collars 28 arranged on the pin as shown. On the outer ends of the pins are arranged operating 'heads or /handles 28 and said pins are also' preferably provided with laterally extending fingers 2 9, which, when the pins are in operative engagement with the recesses 22 'of the disks 20, are engaged with notches 30 in the outer ends of the Acasings and which, when said vpins are retracted and l tu'nd, are engaged with the outer ends of the casings thereby holding said pins in retracted or inoperative position. en pins' 240 are thus retracted the disks 23 and the shafts to which the same are attached may be turned inthe desired di# rect-ion for adjusting the Vplane connected therewith.

In order .to permit both of the shafts V16 and 18, and the planes connected thereto to be operated in unison, I preferably :pro-

vide the shaft 16 with a fixed spur gear 31-and the shaft 18-with a loosely mounted gear 32, said lfears being in operative engagement. The loose gear 32 is provided with' one member 33 of a clutch the other memberr 34 of which is slidably secured to the shaft 18 and is adapted to be shifted into engagement with the clutch member 33 to lock the gear 32 to the, shaft 18 by means of a-short shifting lever 35 which is pivotally secured at its inner end in a V- shaped notch 36 formed in the shaft 18 and projects up through a slot 37 formed in the clutch member 34 as clearly shown in Figs. 5 and 10 ofthe drawings.l lVhen the clutch member 34 is shifted to lock the gear 32 to the shaft 18 the shafts 16 and 18 will be operatively connected together by the gears 31 and 32 so that when either of the shafts are turned by the operating disks hereinbefore described, the other shaft will be simultaneously operated in the opposite direction thus raising or lowering vthe planes in unison.

Revolubly mounted in suitable bearing standards 38 secured to the platform 5 is a propeller shaft 39 having on its rear end a propeller blade 400. Fixed on the inner end of the shaft 39 is a sprocket gear 40 which is connected by a sprocket chain 41 to a sprocket gear 42 loosely mounted on the drive shaft 43 of a suitable motor 44 arranged on the platform 5 as shown. The sprocket gear 42 is fixed on or forms part of a friction clutch member 45 the opposing member 46 of which is slidably keyed to the shaft 43 and is adapted to be shifted b v the lever 47 toengage the same with the clutch member 45 of thelsprocket gear 42 whereby said gear is locked to the shaft 43 andthe movement of said shaft thus imparted to the propeller through the chain 41 and sprocket gear 40;

On the shaft 3 which connects the front ends of the bars 2,'of the frame are a pair of vertically disposed steering Aplanes '48 which are disposed between the central portion of a pair of horizontally disposed steering. planes 49. The planes 48 and 49 are preferably in-the form of .fabric covered frames and the frames of each pair of planes are connected togetherpand spaced apart by suitable cross bars 50 and 51 whereby saidfplanes are braced and firmly secured to theshaft 3. The planes 48 and 49 are adjusted to control thedirection of the machine by means of-,an operating bar orshaft 52 which is pivotally secured inter- Ymediate its ends on a supporting standard 53 by auniversal joint connection 54 Whereby said bar or shaft may be swung in a ver,

i the bar or shaft 52 1s provided with a slotted head 55 whereby'said end of the shaft has a loose sliding connection with a cross bar'56 connecting the rear ends of the planes 48 as xclearly shown in Fig. 6 of the drawings.

To the rear end of the bar 'or shaft 52 is loosely connected ahorizontaltransversely disposed plane securin 4bar 57 Figs. 3, 6, 7 and 8 the opposite' en s of which are slidably engaged with the recessed end bars 58 ol'. -a supporting frame 59 secured to the v upper en d of a supporting standard 60 arranged on the forward'end of the platform .The frame 59 is further held bi suiti Y able brace rods 61 securedthereto an tothe .platform 5 as shown. The bar 57 when thus arranged is adapted to be moved upv and .down or Jlaterally in either direction with fasten the shaft or bar 52 inits/adjusted 1 5 positions `for holding the planes 48 and 49 "Y lat the desired angle by spring clamping plates 62 secured at their upperand lower ends tothe upper'and lower ends of t-he reba'r 57 is engaged, saidplates 62 thus inclosing the ends of the bar 57 in the recesses of the bars 58.. In order to fasten the ends of the bar 57 in the recesses of the bars 58 I provide clamping devices comprisingclam bars 5 8 and the plates 62 and are engaged at their inner ends with clamping blocks 64` which are slidably engaged with the inner sides of the bar 58 and at their outer ends band to bring the cam surfaces thereof into operative engagement with\the spring plates 62 whereby the latter-are clamped into tight 'engagement with the ends of the bar' 57 thus firmly securing said bar inthe position to which it has been moved by the plane-adjusting bar 52. By thus fastening the bar 57 the plane adjusting bar 52 andv the 4 0 steering planes 48 `and 49 will be securely l' locked in their adjustedposition'. -The' innerl end -ofthebar 52 is provided with a Y ysuitable -operating handle which is here shown yin the form 'of a wheel .66. whereb ,51 said bar -mav be rocked` vertically to' tit Ltr-both pairs of `planea- 48- and 49 in a vertical direction whereby thelv machine. is directed bar.' laterally to adjustthe planes 48 in a horigont-al plane whereby the machine may be s teeredto the right 'or left. '1

j LSe'cured to' the'platfoi'm and frame ofthe 'd machine is aflower horizontal. transversely v disposed plane supporting bar 67; Fig. 6 the ends. of which are preferablyconstructed in 1 'skeleton form and 'project a suitable dis.

' ta iice-beyond the `opposite sides of the malchine. The outwardly extending ends of the' lbar 67 are provided withndepending ltjhraekets f 67 0 l and! the bar" isk vpreferably' ypbraced by suitable rods 68-l .secured to said f rackets as shown. the bar 67 near the..

ceterthereof. andv atfitsputer ends .are sevthe movement of the bar or, shaft 52 and is adapted to be secured -when thus moved to cessed bars 58 with which the transverse.

ing bands or rings 63 which will encircle t e engage cam levers. 65 which are adapted. to be turned on the outer ends of 'the links pingft-he air when the 'shafts lpwardly or downwardly-ortosswing said planes-are connected to the shaft 83 byl a seL uredbearingsf 'in-" which is revol'tiblv fixed thereon midway between its ends and 'between the inner bearings 69 a sprocket gear 71which works throu l1 a slot in the bearing 69 and is connecte by a sprocket chain 72 Fig. 4 with a sprocket" gear 73 loosely mounted on the shaft 43 ofthe engine. The gear 73 has formed on one side one member 74 of a clutch, the op cs ing member 75 of whichv is slidably keye to the engine shaft 43 and is adapted to be' shifted 1nto 75 engagement with the clutch member 74 by a suitable clutch shifting lever 76 arranged Vas shown. On .the outer ends of the shaft 70 are fixed bevel Agear pinions 77 the purpose of which will be hereinafter described. 8

Pivotally supported on the.outer ends of the .shaft 70 areshort bearings 78 to the lower sides of which are secured extension bars 671 which are provided with depending angle brackets 7 9 in which are-formed seg mental slots 80. Withthe slots 80 are engaged stop pins81 secured in angle brackets 82 bolted to the under side of the outer ends ofthe bar .67 whereby the pivotal orswin'gf ing movementof the bearings 78 and ehtension bars 671 on the shaft 70 is limited.v Revolubly mounted in the extension bars .671 at the outer ends of the bar 67 are up- 'wardly extending rotary. plane supporting and operating shafts 83 on -the lower ends of whichare fixed bevel gears 84 which areengaged with the bevel gear. inions 77 on the ends of the shaft 70 where y. the movement lplanes or blads86 are preferably arranged 110* in 'series onea-j ve the other lon the shafts- 83 and any. ninber or Iseriesof planes may .be-'providethi two seriesbeing shown in lthe present instance. The upper plane is here 'shown and isv preferably provided with four 7115 `blades or wings, while the lower 'plane is shown as havingbut-two blades or wings.

l.The outer ends of the blades or wings'of.

the lower plane areconnect'ed to thelendsof the adjacentv blades o1 wings' of the upper plane and the ends oft-he blades of both ries ofbra'cing cords or rods 871 p f Securedtoethe .plane supportlnggbars. or

standards near their upperl ends 1s' ahorif 125 zont'al transversely` dispgsed plane support` ing'ba'r 88 the' outer ends of which proyect. beyond the-sides ofthemachine' to a above the upperends of the shafts 83 of the rqfgry planes as shown, 4Fired to the outer if?.

ends of the barn88 are segmental guide frames 8,9 havintgformed in their inner edges guide grooves 90 with which are slidably engaged laterally project-ing guide fianges 91 formed onsegmental rack bars 92 with which the upper ends of the shaft-s 83 of the rotary planes are pivotally engaged as clearly shown in Figs. 12 and 15 of the drawings. By thus connecting the upper ends of the shafts 83 they, together with the rotary planes thereon may be rocked on the ends of the shaft 7 O to bring said planes in the position shown in dotted lines in Fig. 11 whereby the planes are adapted to assist in propelling the machine.

In `order to shift the rack bars 92 and shafts 83 to bring the rotary planes to the desired positions, I provide a suitable shifting mechanism, Figs. 1, 4 and 6 comprising a transversely disposed shaft 93 which is revolubly mounted in suitable bearings 94 arranged on the Abar 88 as shown. On the outer ends of the shaft 93 are fixed spur gear pinions 95 which are adapted to engage the teeth of the rack bars 92 whereby,

when said shaftis revolved in one direction or the other, the rack will be shifted and.

they shafts 83 of the rotary planes thus adjusted to the desired position. Fixedly mounted at a suitable point on the shaft 93 Ais a sprocket gear 94-which is connected by a sprocket chain 95 to a similar gear 96 which is'revolubly mounted on a bearing block 97 securedto one of the bars or standards 7A as shown in Fig. 4f of the drawings.'A y

Secured to one side of the sprocket gear 96 is a crank handle 98 whereby the gear may be turned to operate the shaft 93 and thepinions thereon by which the rotary planes are tilted as hereinbefore described. In order to secure the. rotary planes in their adf justed positions I provide 'the gear 96'with a suitable locking mechanismA comprising a spring projected locking pin 99 which is audapted to be projected through a passage in. the gear and into engagement with one of the series of locking recesses formed in the block'97 in the same manner as shown and described in Fig. 14e of the drawing and de# scribed in connection with the locking mechanism for holding the horizontal planes in their adjusted position.

The bar S8 is suitably main frame and at their upper'endsl to the lower side of the bar 88 as clearly shown in Figs. 1 and 3 of the drawings.- The bar 88 is further braced by inclined brace bars 101 secured thereto and to the upper ends of theV braced by inclined trussed-brace bars 100 which are connected, at their lowerends to the side bars 2 of the.

yable distance above the platform or lower portion of the main frame of the machine whereby the weight of said platform and the parts supported thereon serve as a pendulum for maintaining the center of gravity and keeping the machine in an upright position. The rotary planes valso impart stability to the machine and materially aid in keeping the machine in 'a horizontal position and preventing the same from upsetting in a lstorm, .thus overcoming one of the principal objections and dangers of other forms of air ships now in use.

From the foregoing description taken in connection with# the accompanying drawings, the construction and operation of the invention will be readily understood Without requiring a more extended explanation.

Various changes in the form,.proportion and the minor details of construction may be resorted to without departing from the principle or sacrificing any of the advantages of the invention claimed.

Having thus described my invention, what I claim is: x,

1. A main frame, a pair of planes pivoted at their inner -edges to the main frame, a pair of shafts journaled'in the main frame parallel with the pivots of the planes, a gear on each of said parallel shafts, a rack bar pivoted to each plane and engaging one of said gears, and means for rot ating the shafts to'longitudinally move the rack bars to adjustthe planes on their pivots.

2. In a flying machine, a main supporting frame, a pair of plane supporting standards secured to and. projecting upwardly above said frame, means to connect and brace the. uppr ends of said standards, horizontal sustaining planes hingedly connected at their inner ends to said standards. operating bars pivotally connected at their upper ends to said planes, rack teeth formed on the lower'v ends of said bars, a pair vof plane adjusting shafts, revolubly mounted in suitable bearings on said standards, gears fixedly mounted on the outer ends of said shafts and adapted ,to engage the teeth of said plane adjusting bars whereby the lat- `ter are actuated to swin the outer ends of the planes upwardly 'or d whereby said shafts are revolved to pendently adjust said planes, and means to ownwardly, means indeoperatively connect said shafts together whereby the movement of one shaft will be imparted to the'other and said shafts thus moved in unison to simultaneously adjust said planes.' v

3. In a flying machine, a main supporting frame, a pair of plane supporting standards secured and projectingv upwardly above said frame, means to connect and brace the upper ends of said standards, horizontally sustaining planes hingedlyconnected at their inner ends Vto said standards, operating bars pivt .ot'all-'y connectedi at their upper ends 'tosaid" planes, rackt'eeth formed on'the lower ends of said bars, a-'pair ofy plane adjusting shaftsrevol'ublymounted in suitable bearings on '-1 saidfstandarda'gears fxedly mounted on the 'Y with and. supported by said shaft, a plane operating, rody having a loose sliding conouter ends; of said shafts and adapted to engage the teethof said plane adjusting bars whereby the latter are actuated to swing the outer ends of the planes-upwardly or downwardly, crankdisks Xedly mounted on said shafts, stationary locking disks arranged on said shafts, said disks havin-g formed therein annular. series of recesses, handles arrangedonvsaid crankdisks, spring projected locking pins carried by said' disks and adapted to be engaged with the recesses in saidlocking disks whereby said crank disks andi said shafts are locked when operated 'and to adjust said planes `thereby holding 2Ol the'pl'anes in their adjusted: positions and means tohold said lockingpins in a retractedor .released position.

4.-'. In a flying machine, a main supporting ,frame, apair of plane supporting standards -secured and projecting upwardly above said frame, means to connect and'brace the upper4 the outer ends of the filaires-upwardly or4 downwardly, means toindependently operate said shafts and.ff". tliereby' adjust said planes, a shaft connecting gear xedly mounted on one/ffsaid shafts, a' similar gear loosely mounted lon the other shaft, and engaged with said fixed gear, a clutch mech anism adaptedltolo'ck said loose gear into engagement with its shaft whereby said shaftsI are geared 'together and adaptedto move lin unison, thus simultaneously' adjusting said planes. i

5. In si flying ing frame, horizontally disposed sustaining planes adjustably connected to. saidl frame, a motor arranged on said frame, a rotary propeller operatively connected with said motor, means to throw said propeller into and out of operation, a steering'mechanism, said mechanism comprisinga horizogtally disposed shaft, a pairof parallel vertically disposed steerin planes mounted -1 on said shaft, a pair of horizontally disposed steering' planes'; a rranged above and below said vertical planes midway between their ends, said horizontal planes being connected machine, a main supportv nection at its outer end with the rearends of said verticalplanes, a bar supporting standard, a universal jolnt connection between said bar and said standard,- a plane' securingbar loosely connected to the'lnnerk end ofvsaid operating bar, a supporting' frame havin recessed end bars with which the" outer en s of said securing bar are slid ably engaged, secured to said end'bars, clamps adjustably engaged with the,\recessed end bars of the supporting frame and with said spring clamping plates whereby the latter are actu* atedto clamp the ends of the plane securingv bar thereby fastening said plane operating spring, clamping p'lates bar and steering planes in their adjusted position. A

6. I n a flying machine, a main supporting frame, plane'supporting standards secured to said frame, trussed braces to connect the upper ends of saidfs'tandards to the frame, horizontal sustaining planes .hingedly vconnected to saidl standards, means whereby said planes arfadjusted, a suitably operated .propelling mechanism,. a steering mecha.

nism adapted tosteer said machine in horizontaland vertical planes, a `lower transversely disposed supporting bar having! lts v ends projecting a suitable distance beyond" the opposite sides of the main frame, a plane operating shaft revolubly mounted in suitable bearings on said bar, vplane supportl ing plates pivotally-mounted on the outer ends ofsaid shaft and adjustably secured-to' lthe ends of. said bar, rotaryliftingplanes havingthe lower ends off their shafts revolubly mounted in said plane supporting plates,

,gears xedly mounted on the lower ends of' said shafts, simildr gears xedly mountedpnf the outer endsof sald plane operating shafts whereby sai'dtplanes are driven, and means to adjustably support theupper ends of said" rotary plane shafts whereby :the latter and 4said planes may be adjusted to facilitate the propulsion ofthe machine.

7. Ina flying machine, a main frame, af `transverse bar supported thereon,; bearings fixed on .top of the, outer ends of each bar, .a transverse shaft parallel with the bar.I vmounted .in said bearings, extension bars loosely placed atthe ends of thebar, bearshaft mounted in eachlextension bar lwhereby said vertical shaft and its ysup orting extension bar may 'oscillate4 on -t e parallel yings secured to.' said extension bars and` loosely mounted on the shaft, a vertical" A shaft, bevel gearing connecting each end of the parallel shaft with the lower end of one of the vertical shafts,rot'ary planes secured to the vertical shafts, and means for securing the vertical shafts in' any position to which they may be oscillated.

` 8. In a flying machine,.a main frame, a

.transverse bar supported thereon, bearings fixed on top of the outer ends of said bar, 'a-

transverse shaft parallel with the bar mounted in said bearings, extension bars loosely placed cured to said extension bars and loosely mounted on the shaft, a vertical shaft mounted in each extension bar whereby said vertical shaft and its supporting extension bar may oscillate on the parallel shaft, bevel earing connecting each end of the parallel shaftwith the lower end of one of thevertical shafts, rotary planes'secured to the vertical shafts, and means for securing the verticalshafts in any position to which they may be oscillated, comprising a. bracket depending from each end of the transverse bar, a similar bracket depending from the inner end of each extension bar and bearing against the adjacent bracket on the bar, one bracket of each adjacent pair having a curved slot, and a clamp screw projecting through the curved slot into the adjacent bracket.Y

9. In a flying machine, a main supporting frame, a pair of plane supporting standards arranged thereon, a. transverselydisposed plane supporting bar secured to said main frame and projectin laterally beyond the opposite sides thereo a rotary plane operating shaft revolubly mounted on said bar, plane supportingl plates pivotally mounted on the outer ends of said shaft and loosely connected to the adjacent ends of said supporting bar, al pair 'of rotary lifting and steadylng planes, said planes comprising vertically disposed shafts having their lower ends pivotally mounted in said plates, lifting planes or bladesarranged von said shaft, bevel gears Xedly mounted on the outer ends of said plane operating shaft and engaging the gears on said vertical shft at the ends of the bar, bearings sewhereby the latter and said lifting planes are revolved, an upper plane suppor ing bar secured to the upper ends of said standards, segmental guide frames secured to the outer ends of said upper plane supporting bar, segmental rack bars having a sliding engagement with said guide frames, bearing sockets formed on said rack bars and adapted to receive and revolubly supportthe upper ends of said vertical lifting and steadying plane shafts, a revolubly mounted plane adjusting shaft, gears fixedly mounted on the outer ends of said shaft and adapted to engage and shift said racks in said guide frames to tilt said lifting planes forwardly whereby said planes may be employed to aid in the ropulsion of the machine, a sprocket gear xedly mounted on said adjusting shaft, a bearing block secured to one of said plane supporting standards, said block havin g formed therein an annular series of recesses, a sprocket gear revolubly mounted on rsaid block, a sprocket chain to connect said gear with the sprocket gear on said plane` adjusting shaft, a` crank handle secured to the sprocket gear on said block, and a spring projected lookin pin arranged in said gear and adapted to engaged with one of the recesses in said block whereby said gear is locked and thus' holds said lifting planes in the position to which they have been adjusted by the adjusting shaft gears.

In testimony whereof I have hereunto set my hand in presence of two subscribing witnesses.

REUBEN vB. SVVANK.

Witnesses:

J oHN J. HOOVER, J As. HICKMAN. 

